FR3079265B1 - Support de palier de turboreacteur obtenu par fabrication additive - Google Patents

Support de palier de turboreacteur obtenu par fabrication additive Download PDF

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Publication number
FR3079265B1
FR3079265B1 FR1852557A FR1852557A FR3079265B1 FR 3079265 B1 FR3079265 B1 FR 3079265B1 FR 1852557 A FR1852557 A FR 1852557A FR 1852557 A FR1852557 A FR 1852557A FR 3079265 B1 FR3079265 B1 FR 3079265B1
Authority
FR
France
Prior art keywords
bearing
cone
additive manufacturing
bearing support
turbo
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1852557A
Other languages
English (en)
Other versions
FR3079265A1 (fr
Inventor
Dimitri Daniel Gabriel Marquie
Adrien Jacques Philippe FABRE
Frederic Patard
Pierre Jean-Baptiste Metge
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1852557A priority Critical patent/FR3079265B1/fr
Priority to US16/982,795 priority patent/US11585236B2/en
Priority to PCT/FR2019/050630 priority patent/WO2019180375A1/fr
Priority to CN201980021404.XA priority patent/CN111902611B/zh
Priority to EP19716971.7A priority patent/EP3752719B1/fr
Publication of FR3079265A1 publication Critical patent/FR3079265A1/fr
Application granted granted Critical
Publication of FR3079265B1 publication Critical patent/FR3079265B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162—Bearing supports
    • F01D25/164—Flexible supports; Vibration damping means associated with the bearing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • F01D25/183—Sealing means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/20—Direct sintering or melting
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F10/00—Additive manufacturing of workpieces or articles from metallic powder
    • B22F10/80—Data acquisition or data processing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y80/00—Products made by additive manufacturing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/321—Application in turbines in gas turbines for a special turbine stage
    • F05D2220/3213—Application in turbines in gas turbines for a special turbine stage an intermediate stage of the turbine
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/22—Manufacture essentially without removing material by sintering
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/23—Manufacture essentially without removing material by permanently joining parts together
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/30—Manufacture with deposition of material
    • F05D2230/31—Layer deposition
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/50—Building or constructing in particular ways
    • F05D2230/53—Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece construction
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/50—Bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/98—Lubrication
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
    • Y02P10/00—Technologies related to metal processing
    • Y02P10/25—Process efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Rolling Contact Bearings (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Sliding-Contact Bearings (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)

Abstract

L'invention concerne un support de palier (26), destiné à être solidarisé à un élément fixe de turboréacteur pour supporter un tourillon, comportant un cône (27) qui s'évase depuis une portion centrale (28) de supportage du tourillon vers une portion de solidarisation à l'élément fixe, un organe cylindre (29) prolongeant la portion de solidarisation à l'élément fixe tout en entourant le cône (27), une jupe amont (32) portée par le cône pour délimiter une enceinte amont (33) pour la portion centrale (28), au moins un élément de révolution aval (38, 42) porté par le cône (27) pour délimiter une enceinte aval (39, 43) pour la portion centrale (28). Selon l'invention, ce support de palier (26) est fabriqué en une seule pièce obtenue par fabrication additive.
FR1852557A 2018-03-23 2018-03-23 Support de palier de turboreacteur obtenu par fabrication additive Active FR3079265B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1852557A FR3079265B1 (fr) 2018-03-23 2018-03-23 Support de palier de turboreacteur obtenu par fabrication additive
US16/982,795 US11585236B2 (en) 2018-03-23 2019-03-20 Turbojet bearing support produced by additive manufacturing
PCT/FR2019/050630 WO2019180375A1 (fr) 2018-03-23 2019-03-20 Support de palier de turboreacteur obtenu par fabrication additive
CN201980021404.XA CN111902611B (zh) 2018-03-23 2019-03-20 通过增材制造法生产的涡轮喷气发动机轴承支座
EP19716971.7A EP3752719B1 (fr) 2018-03-23 2019-03-20 Support de palier de turboreacteur obtenu par fabrication additive

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1852557A FR3079265B1 (fr) 2018-03-23 2018-03-23 Support de palier de turboreacteur obtenu par fabrication additive
FR1852557 2018-03-23

Publications (2)

Publication Number Publication Date
FR3079265A1 FR3079265A1 (fr) 2019-09-27
FR3079265B1 true FR3079265B1 (fr) 2020-04-17

Family

ID=62816714

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1852557A Active FR3079265B1 (fr) 2018-03-23 2018-03-23 Support de palier de turboreacteur obtenu par fabrication additive

Country Status (5)

Country Link
US (1) US11585236B2 (fr)
EP (1) EP3752719B1 (fr)
CN (1) CN111902611B (fr)
FR (1) FR3079265B1 (fr)
WO (1) WO2019180375A1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3097900B1 (fr) 2019-06-26 2021-06-04 Safran Aircraft Engines Support de palier de sortie de turbomachine
US11313248B2 (en) 2020-05-05 2022-04-26 Raytheon Technologies Corporation 3-D lattice bearing support structure
DE202021104006U1 (de) 2021-07-27 2021-08-04 MTU Aero Engines AG Lagerkäfig für ein Strahltriebwerk
FR3127262A1 (fr) * 2021-09-17 2023-03-24 Safran Aircraft Engines Détecteur du contact mécanique d’une cage souple radial avec un manchon entourant cette cage dans un palier de turboréacteur
US20240151160A1 (en) * 2022-11-07 2024-05-09 Rtx Corporation Spring damping for bearing compartment
US20240151271A1 (en) * 2022-11-07 2024-05-09 Rtx Corporation Annular oil distributor for bearing chamber
US20240151267A1 (en) * 2022-11-07 2024-05-09 Rtx Corporation Oil passage built into bearing compartment spring
US20240151272A1 (en) * 2022-11-07 2024-05-09 Rtx Corporation Support structure and spring for bearing compartment
US20240151266A1 (en) * 2022-11-07 2024-05-09 Rtx Corporation Thermal zone cooling in a bearing compartment

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2876758B1 (fr) 2004-10-19 2008-04-18 Snecma Moteurs Sa Dispositif de support et de guidage d'un arbre en rotation
US20110278801A1 (en) * 2010-05-11 2011-11-17 Morgan Construction Company Neck seal
ITCO20120059A1 (it) * 2012-12-13 2014-06-14 Nuovo Pignone Srl Metodi per produrre pale cave sagomate in 3d di turbomacchine mediante produzione additiva, pale cave di turbomacchina e turbomacchine
PL402185A1 (pl) * 2012-12-21 2014-06-23 General Electric Company Połączona instalacja ściekowa do silników turbinowych
US20150224743A1 (en) * 2014-02-11 2015-08-13 General Electric Company Additively manufactured article
DE102014208040B4 (de) * 2014-04-29 2019-09-12 MTU Aero Engines AG Lagerkäfig und Lagereinrichtung mit einem derartigen Lagerkäfig sowie Verfahren zum Ausbilden, Reparieren und/oder Austauschen eines solchen Lagerkäfigs
EP3075471B1 (fr) * 2015-03-30 2021-11-03 MTU Aero Engines AG Procédé de fabrication d'une partie de boîtier de turbine à gaz par méthode de fabrication additive
FR3036437B1 (fr) * 2015-05-22 2017-05-05 Snecma Ensemble de turbomachine pour lubrifier un support de palier
US10113483B2 (en) 2016-02-23 2018-10-30 General Electric Company Sump housing for a gas turbine engine
FR3053728B1 (fr) * 2016-07-07 2022-01-21 Safran Aircraft Engines Support de palier en deux pieces
US10436065B2 (en) * 2016-08-18 2019-10-08 United Technologies Corporation Resilient bearing mount with integral damper fluid passage for a geared turbofan engine
FR3056656B1 (fr) * 2016-09-29 2018-12-07 Safran Aircraft Engines Enceinte lubrifiee pour turbomachine d'aeronef, limitant la retention de lubrifiant lors du tangage

Also Published As

Publication number Publication date
EP3752719A1 (fr) 2020-12-23
WO2019180375A1 (fr) 2019-09-26
FR3079265A1 (fr) 2019-09-27
US20210062679A1 (en) 2021-03-04
CN111902611B (zh) 2022-11-08
CN111902611A (zh) 2020-11-06
EP3752719B1 (fr) 2023-02-15
US11585236B2 (en) 2023-02-21

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